Masters Theses

Abstract

"The telecommunications system design goals and functional requirements for an advanced logistic spacecraft are presented qualitatively. Advanced equipment and techniques that meet these system requirements and goals, that are within the state-of-the-art and that are believed to be economically feasible, are enumerated and described. System emphasis is on unification to minimize RF links and antenna subsystems, and on use of functional redundancy to assure satisfactory performance of critical telecommunication functions. The interaction of the telecommunications system design and the spacecraft mechanical, environmental, electrical, and operational interfaces are described in qualitative and quantitative terms. A practical spectrum of system interface characteristics is considered along with the required variations in system design. Considerations in RF system design including ranging code design, system sensitivity models, and RF link margin analysis models are presented. A computer program to calculate RF signal margins and to assist in RF link design of a unified telecommunications system is described in the report and listed in the appendices"--Abstract, Page ii.

Advisor(s)

Crosby, Herbert A., 1926-1992

Committee Member(s)

Newell, John A.
Flanigan, V. J.

Department(s)

Electrical and Computer Engineering

Degree Name

M.S. in Electrical Engineering

Publisher

University of Missouri--Rolla

Publication Date

1969

Pagination

vii, 145 Pages

Note about bibliography

Includes bibliographical references (pages 115-117).

Rights

© 1969 James Myron Romberg, All rights reserved.

Document Type

Thesis - Open Access

File Type

text

Language

English

Subject Headings

Space vehicles -- Communication systemsTelecommunication systems -- Design

Thesis Number

T 2311

Print OCLC #

6013379

Electronic OCLC #

846496401

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